N510UA

Part: ACTUATOR — DEFECTIVE (NLG) · airframe 94,660 hrs · 26,818 cycles

NOSE GEAR DID NOT COME DOWN PER FIM 32-30-00-815-805, NLG LOCK ACTUATOR REQUIRES REPLACEMENT; REMOVED NLG LOCK ACTUATOR PER AMM 32-34-02. INSTALLED NLG LOCK ACTUATOR PER AMM 32-34-02-404-009 EXCEPT STEP 6 DUE TO BAD CASTLE NUT( LP 7983981). REQUIRES OPS AND LEAK CHECKS. ROTABLE PARTS CHANGE WAS INDICATED - TT 1490881 SN OFF 0368 ACTUATOR, ASSY- OFF 75-3232-9-0003 0368 ON 75-3232-9-0003 0613 COMPLIED WITH RII INSP OF INSTALLATION OF NLG LOCK ACTUATOR EXCE PT STEP 6 DUE TO BAD NUT REF LOG 7983981 INSTALLED BOLT, WASHER, CASTLATED NUT, AND COTTER PIN PER AMM 32-34-02-404-009 STEP E (6) ON THE LOCK ACTUATOR FOR THE NOSE LANDING GEAR. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD. GEAR EXTENTION AND RETRACTION TEST GOOD. C/W RII INSP OF STEP E6 AS WELL AS LEAK CHECK, OPSCHECK AND GEAR SWING. ALL WAS SATISFACTORY

Part: STRAP — CORRODED (APU BAY) · airframe 94,380 hrs · 26,763 cycles

(B757-49-38083) TAIL COMPARTMENT ACCESS THROUGH 311AL APU INLET DOOR AT STA 1787 HAS CORROSION UNDERNEATH NUTPLATES AS MARKED. ( 068-022) REMOVED EXFOLIATED STRAP AND REPLACED WITH P/N 75-2098-3-3013 (1 48N3138-20) PO NO: TUA 00001297 AT APU INLET DOOR STA 1787 BETWEEN STR. 3R-STR 6R IAW SRM 51-40-02 PARA. 4B AND DWG 148 N3105. WORK ACCOMPLISHED AND INSPECTED. INSPECTION COMPLETED AND ACCEPTED.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 94,380 hrs · 26,763 cycles

FWD CARGO DOOR LOWER EDGE BEAM GOUGED. REMOVED AND REPLACED EDGE BEAM AT FWD CARGO DOOR LWR SIDE IAW SRM 51-40-02 PAGE 2 PARA 4B AND IPC 52-34-01-05 AND DWG 143N6603. WORK ACCOMPLISHED AND INSPECTED. INSPECTION COMPLETED AND ACCEPTED.

Part: STRUCTURE — GOUGED (FWD CARGO DOOR) · airframe 94,380 hrs · 26,763 cycles

FWD CARGO DOOR, FWD CORNER WAS GOUGED ON THE LOWER SIDE. REMOVED AND REPLACED THE CORNER IAW SRM 51-40 -02, PG7 AND PG31.

Part: SLIDE — NO TEST (R4 DOOR) · airframe 94,380 hrs · 26,763 cycles

R4 DOOR ESCAPE SLIDE OPERATIONAL CHECK FAILED.

Part: LAMP — ABNORMAL (EMERGENCY LIGHT) · airframe 91,415 hrs · 26,195 cycles

L2 SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED CHECKED NORMAL.

Part: UNKNOWN — UNKNOWN (DOOR SLIDE) · airframe 90,875 hrs · 26,087 cycles

EMERGENCY EXIT SLIDE LIGHT WILL NOT COME ON. CYCLED THE DOOR ARMING LEVER SEVERAL TIMES. OPS CHECKED GOOD.

Part: EXTINGUISHER — MALFUNCTIONED (LAVATORY) · airframe 90,806 hrs · 26,072 cycles

LAVATORY FIRE EXTINGUISHING LAVATORY SMOKE ALARM ACTIVATED BY SMOKE, AUTOMATIC FIRE EXTINGUISHER DID NOT DISCHARGE AND TEMP INDICATOR STILL GRAY, LEFT AFT LAVATORY ALARM ACTIVATED BY SMOKE FROM GALLEY, OPERATES NORMALLY. OK TO CONTINUE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 90,045 hrs · 25,926 cycles

PASSENGER COMPARTMENT ILLUMINATION REPORT EMERG WINDOW (SIDEWALL) LIGHTS SYMPTOMS OR PATTERNS ALONG WITH FAULT CODE SIDEWALL LIGHTS AT ROWS 20/21 ON BOTH SIDES FLICKER ON/OFF. REPLACED EMERGENCY EXIT DOOR LAMPS AT SEATS 20-21 CDE OPS CHECKED NORMAL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,043 hrs · 25,732 cycles

CRACK ON THE MAIN CABIN FLOORBEAM UPPER CHORD AT RADIUS BS 700 LBL 24.75 & LBL 45.5. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBEAM UPPER CHORD BS 700 LBL 24.75 IAW ECRA NR 5310-07069

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 89,043 hrs · 25,732 cycles

CRACK ON THE MAIN CABIN FLOOR BEAM UPPER CHORD AT RADIUS, BS.660 LBL.45.50. REPAIRED PER ECRA 5310-07070.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,043 hrs · 25,732 cycles

STA 503 BETWEEN STR 27R AND 28R, FOUND DENT WITH GOUGE. REPAIR REQUIRES EVALUATION FOR PERMIT REPAIR WITH SOLID RIVETS AND REMOVED AND REPLACED INCOMING TEMPORARY REPAIR BS503 BETWEEN STR 27R AND STR 28R IAW ECRA NR 5330-05944.

Part: BRACKET — CORRODED (BS 680) · airframe 89,043 hrs · 25,732 cycles

FWD CARGO FRAME BS 680 LBL4, CORROSION ON VERTICAL SUPPORT. REMOVED AND REPLACED VERTICAL SUPPORT IN FWD CARGO FRAME B.S. 68 0 LBL 4 IAW B-757-200 SRM 51-40-02 PAR 4, FIG 8 & 51-40-02 PAR 7 D, FIG 12. REMOVED DOT. WORK PERFORMED AT HAECO MCN. INSP BY QC 76. V892627

Part: FLOORBEAM — CRACKED (BS 700) · airframe 89,043 hrs · 25,732 cycles

TWO CRACKS ON THE MAIN CABIN FLOORBEAM FWD SIDE ATTACH ANGLE AT BS 700 LBL 24.75. REMOVED & REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, PARA 7, FIG 12,

Part: FLOORBEAM — CRACKED (BS 700) · airframe 89,043 hrs · 25,732 cycles

MAIN CABIN FLOORBEAM BS 700, LBL 45.5 IS CRACKED AT TOP. REMOVED & REPLACED THE FLOOR BEAM ATTACH ANGLE IAW SRM 51-40-02, PARA 7, FIG 12.

Part: ANGLE — DAMAGED (BS 780-800) · airframe 89,043 hrs · 25,732 cycles

INTERCOSTAL WEB IN MAIN CABIN FLOOR AT BS 780-800 BL0 HAS ELONGATED HOLES. INTERCOSTAL WEB WAS REMOVED AND REPLACED ON 28744 LP.

Part: ANGLE — CRACKED (BS 780-800) · airframe 89,043 hrs · 25,732 cycles

FWD CARGO CEILING WEB ANGLE IS CRACKED BETWEEN BS 780 - 800, BL 0. REMOVED & REPLACED THE WEB & ANGLE IAW SRM 51-40-02, PAR 7, FIG 12.

Part: SWITCH — FAULTY (R4 DOOR) · airframe 88,652 hrs · 25,656 cycles

NR 4 RT MED ARM/DISARM WARNING LIGHT INOP. REPLACED SLIDE ARM SW S10225 REF MM 25-66-11, CKS GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 85,161 hrs · 24,973 cycles

VENT ASSEMBLY, PN 214N2520-59, ABOVE SEAT 38A, ATTACH HOLES BROKEN OFF. REPAIRED DAMAGED HOLES.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 84,908 hrs · 24,924 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 1 - 4 AISLE & 20 - 24 AISLE, USING DOOR TEST SWITCH. R & R 2B EMER PATH LIGHT CONNECTORS IAW SWP 20-61-28. PERFORMED OPERATIONAL CHECK OF SYS WITH NO DEFECTS.

Part: FCU — FAULTY (NR 1 ENGINE) · airframe 83,705 hrs · 24,692 cycles

ENGINE 1 ENG VLV LIGHT CAME ON DURING FLIGHT, ALL ENG PARAMETERS WERE NORMAL. VLV WENT OFF AT SHUTDOWN. REPLACED RELAYS K10462 & K10463 PRECAUTIONARY. WHILE ACCOMPLISHING FIM 76-11-00 BLOCK 1, 11,21 PG 110, FOUND FUEL CONT UNIT CONN PARTIAL. REPLACED NR 1 ENG FUEL CONT IAW AMM 73-21-01-401. OPERATIONS & LEAK CHECKED GOOD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,160 hrs · 24,588 cycles

CABIN FLOORBEAM STABILITY STRAP REPAIR CRACKED AT BS 365.25, LBL 25.5. REPAIRED CABIN FLOORBEAM STABILITY STRAP BS 365.5, LBL 25.5 IAM SRM 53-00-51 REPAIR 13.

Part: OVEN — DIRTY (GALLEY) · airframe 82,711 hrs · 24,501 cycles

AFT OVEN IN THE MID GALLEY HAD AN ODOR. CREW SUGGESTED THAT THERE WAS SPILLED CARAMEL OR OTHER FOOD THAT WAS THE CAUSE. R & R OVEN. SMOKE WAS CONTAINED TO THE OVEN ONLY IAW CREW BRIEF.

Part: BEARING — WORN (RT ELEVATOR) · airframe 80,290 hrs · 24,040 cycles

RIGHT ELEVATOR OTBD PCA IDLER LINK INBD BEARING WORN HAS APPROXIMATELY .070 RADIAL PLAY. LIMIT IAW MM 27-31-05 P G 601 .003 INCH. REACTION LINK TRUNION BEARING SPINS IN TRUNION HOUSING.

Part: PROCESSOR — FAULTY (FUEL SYSTEM) · airframe 78,761 hrs · 23,752 cycles

FUEL QTY CHANNEL STATUS MESSAGE ON EICAS. REPLACED FUEL QTY PROCESSOR CHECKED GOOD.

Part: WIRE — BROKEN (R4 DOOR) · airframe 78,711 hrs · 23,743 cycles

R4 DOOR SLIDE INDICATION IS WEAK. CLEANED CONTACTS, NO HELP. TRIED ANOTHER LED LENS CAP, NO HELP. NEED LIGHT ASSEMBLY PCN 561-2342. REPAIR IAW WDM 25-66-11, FOUND WIRE 3682-E-PA BROKEN OFF NEAR SPLICE AT PROXI SW S10224. REPAIRED WITH ENVIRONMENTAL SPLICE IAW SWPM 20-30-12, SYSTEM OPERATIONS CHECKED OKAY.

Part: LENS — DIRTY (R4 DOOR) · airframe 78,636 hrs · 23,729 cycles

DOOR ARM LIGHT INOPERATIVE AT 4R, LIGHT WORKS BUT IS DIM. CLEANED LENS & SWITCH CONTACTS. AFTER CLEANING OPERATED SEVERAL TIMES & CHECKED OKAY.

Part: COVER — MISSING (CABIN) · airframe 78,621 hrs · 23,726 cycles

LT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REPLACED LT SIDE OVERWING EXIT SIGN LENS COVER.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 78,578 hrs · 23,718 cycles

NR 2 ENG, CRACK INDICATED DURING HFEC INSPECTION ON SEVEN EACH BLADES' LE. REPAIRED IAW MM 72-31-02, OKAYED FOR SERVICE.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 78,440 hrs · 23,690 cycles

FUEL QUANTITY CHANNEL STATUS MESSAGE DISPLAYED ON EICAS.

Part: NOSE COWL — DENTED (RT ENGINE) · airframe 78,402 hrs · 23,683 cycles

DENT IN RT ENGINE NOSE COWL. DAMAGE AT 7 O'CLOCK IN LENGTH, 2 IN WIDTH, 0.062 5 DEPTH. DENT ON NOSE COWL LE LIP. DENT SMOOTH & FREE OF SHARP CREASES OR CRACKS, AREA WITHIN LIMIT IAW SRM 54-11-01 P201 & GMM 06-35-05.

Part: TERMINAL — SHORT (L2 DOOR) · airframe 78,209 hrs · 23,645 cycles

PRIOR TO DEPARTURE FLT CREW FOUND BREAKER R34 POPPED. REPAIRED SHORTED TERMINAL LUGS ON L405 L2 DOOR GIRT BAR ANNUNCIATOR LT IAW WDM 25-66-11. OPERATIONS CHECKED OKAY.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 77,375 hrs · 23,477 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE INFLATION CYLINDER PRESSURE INDICATOR IS IN THE RED BAND. INSTALLED R1 DOOR SLIDE IAW AMM SUA 25-66-01.

Part: FRAME — CORRODED (BS 1701) · corrosion level 2 · airframe 77,375 hrs · 23,477 cycles

FRAME BS 1701 CORRODED BETWEEN S9-10R. REMOVED DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR ANGLE.

Part: STRINGER — DAMAGED (BS 1701 S23L) · corrosion level 2 · airframe 77,375 hrs · 23,477 cycles

CORROSION ON STRINGER 23L AT BS 1701. REMOVED DAMAGED SECTION OF STRINGER 23L1. INSTALLED STRINGER SPLICE IAW SRM 51-04-02. MAJOR REPAIR.

Part: SKIN — DENTED (BS 440) · airframe 77,375 hrs · 23,477 cycles

DENT AT BS 440, BETWEEN S28-29R. REMOVED DAMAGED SKIN, INSTALLED REPAIR DOUBLER AT BS 439.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,375 hrs · 23,477 cycles

DENT IN FUSELAGE SKIN ABOUT 3 INCHES AFT OF LOWER AFT CORNER OF CARGO DOOR. DENT IS ABOUT 5 BY 2.5 INCHES AND ABOUT.250 IN DEPTH. FOUND WITHIN SRM LIMITS, HFEC INSPECTED SKIN, HOLES, AND INTERNAL STRUCTURE NO CRACKS NOTED. OVERSIZED AND INSTALLED FASTENERS IAW EA 57-5361-13-A0977 AND 8110-3 OK AS PERMANENT REPAIR.

Part: RADOME — DAMAGED (NOSE) · airframe 77,135 hrs · 23,430 cycles

DURING LIGHTNING STRIKE INSPECTION, FOUND RADOME LOWER SECTION DAMAGED. REPAIRED 3EA DAMAGED AREA PER SRM REPAIR 6 PARAGRAPH 4.

Part: ADC — FAULTY (NR 1) · airframe 76,086 hrs · 23,229 cycles

AIRSPEED INDICATOR DISAGREE, FLIGHT DIVERTED. TRIPPED ON LEFT STAB TRIM & ELEV LIMIT MODULE. REPLACED LEFT ADC AND RESET LEFT SAM.

Part: FITTING — DIRTY (GIRT BAR) · airframe 75,870 hrs · 23,189 cycles

1R UNABLE TO ARM. CLEANED GIRT FITTINGS, OPS GOOD.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 75,247 hrs · 23,068 cycles

DOOR 2R STILL HAS LOUD SQUEAL. REPEAT GRIPE. THIS IS 6TH WRITE-UP IN 8 DAYS. FOUND AFT DOOR SILL SCUFF PLATE CRACKED IN 2 PLACES. REPAIRED SILL SCUFF PLATE PER MM. PRESSURIZED CABIN, LEAK CHECK GOOD.

Part: SKIN — CORRODED (RT WING) · airframe 74,325 hrs · 22,890 cycles

RIGHT WING UPPER SURFACE HAS CORROSION FROM RT WBL 75 TO RT WBL 135 AND FROM STGR 19 TO AFT SPAR. REF SCAL LP 996 8573. COMPLIED WITH ECRA 5720-0 2300. SCAL 09882 INSP SCAL 00535.

Part: SKIN — DENTED (BS 1445 S24-26R) · airframe 74,325 hrs · 22,890 cycles

SKIN DENTED BS 1445 BETWEEN S24 AND 26R. INSTALLED INTERIM REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 1681-1691) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

SUB FLOOR CORRODED AND LIFTED UP BS 1681 RBL 38 TO RBL 56. INSTALLED DECK PLATE SPLICE REPAIR BS 1681-1691 AND LBL60-RBL60.

Part: SKIN — DENTED (BS 1445) · airframe 74,325 hrs · 22,890 cycles

SKIN DENT BS 1445 BETWEEN S24 AND 26R. ACCOMPLISHED INTERIM REPAIR PER ECRA 5330-04238.

Part: SKIN — DENTED (BS 1445) · airframe 74,325 hrs · 22,890 cycles

SKIN DENTED BS 1445 BETWEEN S24 AND 26R. INSTALLED INTERIM REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

FLOORBEAM TEE CAP CORRODED STA 1640 LBL 32 RBL 61. INSTALLED UPPER TEE REPAIR TO BS 1640 FLOORBEAM REF ECRA 5310-05493.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 74,325 hrs · 22,890 cycles

BS 324 FLOORBEAM HAS CORROSION BETWEEN RBL 45 AND 55. INSTALLED INTERIM REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

BS 1681 FLOORBEAM UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM BS 1681. REF. SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 310) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

BS 310 FLOORBEAM HAS CORROSION AT RBL 40. FABRICATED AND INSTALLED ANGLE AND STRAP REPAIR IN REF TO ECRA 5310-05501.

Part: FLOORBEAM — CORRODED (BS 365 RBL 48) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

FLOORBEAM CORRODED STA 365 CENTERLINE TO RBL 48. PERFORMED A PARTIAL CHORD REPLACEMENT REF ECRA 5310-05496.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 74,325 hrs · 22,890 cycles

STA 1661 FLOORBEAM HAS CORROSION LBL 33 TO RBL 21. CUT OUT DAMAGED AREA AND INSTALLED REPAIR REF SRM 53-00-51 RPR 3. MAJOR REPAIR

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 74,325 hrs · 22,890 cycles

LEFT HORIZONTAL STABILIZER HAS A DENT ON BOTTOM SURFACE ABOUT 3-16" DEEP BY 2.5" IN DIAMETER. LOCATION IS ABOUT 1.5 FEET AFT OF LEADING EDGE & ABOUT 6 FEET OUTBOARD OF FUSELAGE. FOUND DAMAGE HAS NO PROGRESSION AND WITHIN LIMIT PER SRM. REF SCAL LP 9667259 FOR REPAIR INSTALLED PER SRM 51-70-10.

Part: COMPUTER — FAULTY (ELEVATOR FEEL) · airframe 73,986 hrs · 22,824 cycles

FLEW THIS AIRPLANE FOR 2 LEGS. BOTH THE CAPT AND F/O FELT THE A-C WAS VERY NOSE HEAVY ON T/O. REPLACED ELEVATOR FEEL COMPUTER PER MM, OPS & LEAK CHECKS ARE GOOD.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 73,853 hrs · 22,799 cycles

NR 1 ENGINE FOUND 3EA FAN BLADE DAMAGED BEYOND REPAIR BLADES ARE NOT NUMBERED. FOUND AN 8" FILE AGAINST EXIT FAN CASE STATOR VANES AT 5:30 POSITION. ON ARRIVAL TO JFK FOUND 3 BLADES ON NR 1 ENG DAMAGED FOUND 8 INCH FILE IN COWL ALSO MISC OTHER DAMAGE BUT REPAIRABLE. PHOTOS ADDED TO RVI, BLADES COMING AOG N6678 FROM SFO FLT - 824. BLADES CONFIRMED ON FLT. REPLACED DAMAGED BLADES IN MATCHED MOMENT SETS IAW.

Part: LENS — LOOSE (CABIN) · airframe 73,616 hrs · 22,753 cycles

THE 9D EMERGENCY EXIT LIGHT LOOSE. SECURED 9D EXIT LIGHT LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,132 hrs · 22,661 cycles

OVERWING FWD EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,708 hrs · 22,580 cycles

SEATS AT ROW 5AB AND 9AB EACH HAVE ONE EEL LAMP INOP, NEEDS LIGHT ASSY NIL STOCK SFO. REPLACED LIGHT ASSY BOTH POSITIONS OP CHECKED OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 72,221 hrs · 22,486 cycles

SEAT 18C 23C AND 9B EMERGENCY LIGHT OUT DURING TEST. SECURED LOOSE CONNECTORS AT SEATS 18C & 9B AND INSTALLED NEW LIGHT STRIP AT SEAT 23C, EEL LIGHTS OP CHECK NORMAL PER MM.

Part: PROBE — DEFECTIVE (FUEL TANK) · airframe 71,875 hrs · 22,417 cycles

CTR TANK QTY FLUCTUATIONS. REPLACED LT CENTER TANK NR 3 PROBE. PREP TO ACP.

Part: CAP — SHORTED (EVAC SLIDE) · airframe 71,603 hrs · 22,362 cycles

OFF WING ESCAPE SLIDE RT SYS PRESS BOTTLE SQUIB DISCONNECTED AND SHORTING CAP INSTALLED AND SAFETY PIN INSTALLED IN MASTER CONTROL VALVE. REINSTALLED CONN AND REMOVED PIN AND SHORTING CAP PER MM. ACCOMPLISHED INSPECTION PIN REMOVED AND STOW PRESSURE GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 70,869 hrs · 22,216 cycles

FOUND 1 RT DOOR SLIDE BOTTLE PRESSURE IN RED. REPLACED IR DOOR SLIDE PER MM OPS CHECK NORMAL. 1R MED SLIDE PERFORMED RII INSPECTION OF SLIDE INSTALLATION ASSY. NO DEFECTS FOUND.

Part: VALVE — MALFUNCTIONED (FUEL CROSSFEED) · airframe 69,820 hrs · 22,009 cycles

FUEL IMBALANCE, FLIGHT DIVERTED. CREW REPORTED FUEL IMBALANCE BETWEEN THE LT AND RT MAIN TANKS IN CRUISE. IT APPEARED THE RT MAIN TANKS WERE SUPPLYING FUEL TO BOTH ENGINES WITH CROSSFEED VALVE CLOSED AND CTR TANK EMPTY. INITIALLY HAD 1300 LB IMBALANCE WITH FUEL CONFIGURATION LIGHT ON, AND 19 MINS LATER THE IMBALANCE HAD INCREASED TO TO 4000 LBS. AIL TRIM REQ 1 UNIT OF RT WING DOWN. ENG FF WERE MATCHED AND TOTALIZER & ALC TOTAL MATCHED. IAW SFOLM, REPLACED FUEL CROSSFEED VALVE WITH WORKING APU FUEL SHUTOFF VALVE. ALSO WILL INOP APU DUE TO VALVE SWAP.

Part: CONTROL VALVE — FAULTY (CABIN PRESSURE) · airframe 69,430 hrs · 21,935 cycles

BLEED & CABIN PRESSURE ISSUES. FLIGHT DIVERTED. REPLACED LEFT PACK TEMP CONTROL VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,627 hrs · 21,780 cycles

EMERGENCY LIGHT AT SEAT 18 AND 19 INOPERATIVE. REPLACED EMERGENCY LIGHT STRIPS, OPS OKAY.

Part: BATTERY — FAULTY (MASTER) · airframe 68,106 hrs · 21,678 cycles

MAIN BATTERY CHARGER STATUS REAPPEARED AFTER 2 HRS OF FLT. REPLACED MAIN SHIP BATTERY AND OPERATION CHECKS GOOD IAW MM.

Part: CHARGER — FAULTY (MASTER BATTERY) · airframe 68,100 hrs · 21,677 cycles

MAIN BATTERY CHARGER EICAS. REPLACED MAIN BATTERY CHARGER AND TIGHTENED BATTERY TERMINALS, OPS CHECKS OK.

Part: COVER — UNSECURE (EVAC SLIDE) · airframe 67,894 hrs · 21,636 cycles

RT OVERWING EXIT SLIDE COVER NEEDS TO BE RE-SECURED. REMOVED AND REPLACED RT OVERWING EXIT SLIDE.

Part: LAMP — INOPERATIVE (FIRE HANDLE) · airframe 67,687 hrs · 21,596 cycles

NR 2 ENGINE FIRE HANDLE LIGHTS INOP DURING FIRE TEST, (LIGHTS INSIDE FIRE HANDLE NOT LIGHTING UP). RELAMPED NR 2 ENGINE FIRE HANDLE, OPERATIONS CHECKED NORMAL IAW MM OPS TEST.

Part: SKIN — DAMAGED (BS 670 S14-19L) · airframe 67,687 hrs · 21,596 cycles

LT SIDE OF FUSELAGE DAMAGED. DAMAGE CAUSED IS A APPROX 5 FT LONG GOUGE APPROX 2FT FWD OF DOOR 2L. DAMAGE CAUSED BY RT FWD STANCHION ON CARGO KING. ACCOMPLISHED PERMANENT REPAIR IAW EVA-73780 ON OV WU K1222G.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 67,681 hrs · 21,595 cycles

BURNING SMELL ON FLIGHT DECK. WINDSHIELD 1L CRACKED AND BURNED. FLIGHT DIVERTED. REMOVED WINDSHIELD 1L.

Part: UNKNOWN — ODOR (CABIN) · airframe 67,674 hrs · 21,592 cycles

ELECTRICAL ODOR, FLIGHT DIVERTED. CONDUCTED THOROUGH INSP OF WIRING IN OVEN AREA, NO BURNED ELECTRICAL ODOR NOTED. FOUND WIRING IN GOOD CONDITION. APPLIED POWER TO OVENS, COFFEE WARMERS AND COFFEEMAKERS FOR 1 HOUR. E&E COMPARTMENT ODOR OK. WINDSHIELD 1L CRACKED AND BURNED. REMOVED WINDSHIELD 1L.

Part: SKIN — DAMAGED (RUDDER) · airframe 67,360 hrs · 21,532 cycles

FOUND EVIDENCE OF LIGHTNING STRIKE EXIT. T/E AT TOP OF RUDDER TO 48 IN DOWN HAS MULTIPLE DAMAGE STRIKES AND DAMAGED FASTENERS AND FIBER DAMAGE WITH DELAM APPROX 6 IN FWD OF T/E ON LT SIDE UPPER CONDUCTIVE FRAME HAS BURNED AND PULLED FASTENERS AT REAR SPAR ATTACH POINT. RT SIDE APPROX 20 IN FROM TOP HAS DELAM AND PEELING CARBON FIBER APPROX 100 SQ" IN NON CRITICAL AREA. MULTIPLE STATIC WICK BAS (PARTIAL). REMOVED RUDDER IAW MM. R & R TO SHOP 271 UNDER R38097. ACCOMPLISHED REF MM. COMPLETED RUDDER INSTALLATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,253 hrs · 21,511 cycles

SEAT MOUNTED EEL INOP AT SEAT 18 ABC. REPLACED LIGHT ASSY, OP NORMAL.

Part: MECHANISM — LACK OF LUBE (R1 DOOR) · airframe 67,179 hrs · 21,497 cycles

DOOR 1R WILL NOT DISARM. REMOVED LINER. ADJUSTED & LUBED ARMING MECHANISM. OPS CHECK NORMAL. ACCOMPLISHED INSPECTION OF DOOR 1R ARMING MECHANISM AFTER ADJUSTMENT AND LUBING.

Part: ELEVATOR — DAMAGED (LEFT) · airframe 67,169 hrs · 21,495 cycles

LEFT ELEV HAS DAMAGE. ACP LT ELEVATOR FREEPLAY CHECK. NO DISCREPANCIES FOUND. REPLACED LT ELEVATOR. INSPECTED SAFETY AND SECURITY OF LT ELEVATOR RIG AND OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 66,718 hrs · 21,407 cycles

EMERGENCY LIGHT WIRES CUT ON WALL ACROSS FROM 1L CLOSET. NEED TO HAVE FEMALE PLUG SPLICED TO BE ABLE TO CONNECT NEW EMERGENCY LIGHT THAT WAS INSTALLED. CUT IS IN FLAT WIRE, WILL NEED NEW LIGHT ASSY. PARTS NEEDED 5879-1 AND 5863-1 LEAD IN CABLE. REPAIRED EMERGENCY LIGHT WIRE AT FWD CABIN DIVIDER RT SIDE. EMERGENCY LIGHT, OPS CK GOOD.

Part: GROUND WIRE — LOOSE (GALLEY) · airframe 66,708 hrs · 21,405 cycles

F/A RECEIVED SHOCK FROM TOUCHING METAL IN MID GALLEY. DEACTIVATED MID FWD GALLEY BOTH COFFEEMAKERS & MID FWD GALLEY COFFEE WARMER, NO SHOCK FELT. BOTH COFFEEMAKERS COLLARED. FOUND G2A GALLEY COUNTER & G2B GALLEY COUNTERS NOT GROUNDED. FOUND G2A COUNTER AT 36VAC WHEN COFFEEMAKER M21 TURNED ON. REPLACED M21. NOW COUNTER AT 0.086VAC WITH M21 ON. REPAIRED GROUND ON GALLEY COUNTER G2B, ALL ITEMS IN GALLEY ARE GROUNDED. GROUND ON GALLEY COUNTER G2B HAS BEEN REPAIRED. ALL ITEMS IN GALLEY ARE GROUNDED AND NO STRAY VOLTAGE WAS MEASURED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,859 hrs · 21,242 cycles

AFT LT DOOR NR 3 EMERGENCY DOOR LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MISSING (SEAT 16C) · airframe 65,535 hrs · 21,180 cycles

SEAT MOUNTED EMERGENCY ESCAPE LIGHT SEGMENT MISSING. LOWER PART OF AISLE ARMREST OF SEAT 16C. REPLACED EMERGENCY LIGHT SEGMENT AND OPS CHECKS NORMAL.

Part: DUCT — DAMAGED (AC PACK) · airframe 65,363 hrs · 21,147 cycles

CABIN PRESSURE ISSUE, FLIGHT DIVERTED. R ENG PRSOV "OFF" LT NOT ILLUMINATED. WITH ISOLATION VLV CLOSED APU AIR IS AVAIL FOR L ENG START AND PACK OPERATION. DUE TO INABILITY TO MAINTAIN CABIN PRESS ON SINGLE PACK, ACCOMPLISH INTENSIFIED INSPECTION OF BOTH PACK BAYS FOR POSSIBLE DUCT LEAK. FOUND FLEX HOSE & CLAMP BLOWN OFF A-C DUCT. FLEX HOSE RE-INSTALLED ON LT PACK DUCTING ALONG WITH CLAMP. LEAK CHECKED NORMAL. ACCOMPLISHED ENGINE RUN. INDICATIONS AND OPERATION NORMAL. APU PNEUMATICS NORMAL TRIED TO BACK PRESS THE RT ENG PRSOV CLOSED WITH EXTERNAL AIR REF SERVICE TIP. NO JOY. LIKELY NEEDS PRSOV REPLACEMENT. REPLACED PRSOV. PRESSURIZED A/C. PRESSURIZATION NORMAL WITHOUT FLUX IN CABIN PRESSURE. ACCOMPLISHED ENGINE RUN. INDICATIONS AND OPERATION NORMAL. APU PNEUMATICS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,903 hrs · 21,046 cycles

EEL LIGHT ASSY IS INOP AT SEAT ROW 20AB. REPLACED EMERGENCY LIGHT ASSY & OPS CHECKED OKAY.

Part: LIGHT — BROKEN (CABIN) · airframe 64,496 hrs · 20,967 cycles

EMERGENCY LIGHTING ON FLOOR NEAR 9B IS BROKEN. RESECURED LIGHT ASSY AND OP CHECKED EMERGENCY LIGHTS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,434 hrs · 20,955 cycles

EMERGENCY AISLE LIGHT ABOVE SEAT 26D IS INOP. RELAMPED EMERGENCY LIGHT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 63,390 hrs · 20,757 cycles

ENGINE FUEL LEAK INDICATION. FLIGHT DIVERTED.

Part: VALVE — LEAKING (FUEL CROSSFEED) · airframe 63,390 hrs · 20,757 cycles

ENGINE FUEL LEAK INDICATION. FLIGHT DIVERTED. REPLACED FUEL CROSSFEED VALVE. ADDED FUEL AND DRIPPED TANKS BOTH WITHIN TOLERANCE.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 62,801 hrs · 20,645 cycles

FUEL FILTER BYPASS MSG. FLIGHT DIVERTED. REPLACED FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH, LEAK CK AND OPS OK. REPLACED FUEL FILTER BYPASS CONNECTOR D5004 AND ACCOMPLISHED ENG RUN. SYSTEM OPS CHECKS SATISFACTORY.

Part: OXYGEN BOTTLE — MISINSTALLED (CABIN) · airframe 62,108 hrs · 20,514 cycles

ALL PORTABLE O2 CYLINDERS IMPROPERLY STOWED. STRAPS ARE CAUGHT UNDER CLAMPS. SECURED O2 BOTTLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,029 hrs · 20,499 cycles

FOUND DENT AND GOUGE JUST AFT OF DOOR 2 LEFT, ON LOWER RIGHT CORNER, AT STATION 760, 8.5 INCHES UP OF WATER LINE. LENGTH OF GOUGE IS 2 INCHES LONG AND DENT WIDTH IS 1 INCH WITH A DEPTH OF .062 DEEP. CLEANED AREA, AND SMOOTHED AREA. AREA IS FREE FROM CRACKS AND CREASES REF SRM 53-00-01. ALSO APPLIED ALODINE. MF3398 CREATED TO MONITOR. OK FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (RIGHT) · airframe 61,827 hrs · 20,457 cycles

PRESSURIZATION PROBLEMS. FLIGHT DIVERTED. FOUND RT ENGINE HPSOV FAILED. REPLACED RT HPSOV. OPS AND LEAK CHECKED. NO DISCREPANCIES NOTED. BLEED SHIFT OPS NORMAL.

Part: WEB — WORN (NR 2 PYLON) · airframe 61,823 hrs · 20,456 cycles

NR 2 PYLON HYD PRESSURE LINE FITTING AT PYLON STRUT WALL, PYLON SKIN WEB IS WORN. REPAIRED PYLON.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,638 hrs · 20,419 cycles

OUTSIDE SLIDE LIGHT IS INOP AT DOOR 4L. *S/D* REPLACED M10818 POWER SUPPLY BATTERY ASSY, OP CHECKS OKAY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,638 hrs · 20,419 cycles

LT SIDE MOST TWO AFT EMERGENCY LIGHTS OVERHEAD STOW BIN NO GOOD DURING CHECK. RELAMP, NO HELP. FURTHER TS NEEDED. *S/D* REPLACED M10818 POWER SUPPLY BATTERY ASSY, EMERGENCY LIGHTS OP CHECKS OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,691 hrs · 20,241 cycles

EXIT IDENTIFIER SIGNS - VERTICLE EXIT LIGHTS INOP DOOR 2L AND 2R, POSSIBLE BAD INVERTER. CONNECTOR WAS LOOSE RESEATED CONNECTOR. ALL LIGHTS OK.

Part: LIGHT — LOOSE (L3 DOOR SLIDE) · airframe 60,328 hrs · 20,173 cycles

FOUND DOOR 3L SLIDE ARMED LIGHT INOP. FOUND LIGHT ASSY LOOSE. SECURED LIGHT ASSY AND ARMED DOOR AND LIGHT CAME ON.

Part: PROCESSING UNIT — FAULTY (FUEL SYSTEM) · airframe 59,141 hrs · 19,947 cycles

FLIGHT DIVERTED DUE TO A FUEL QUANTITY PROBLEM. FUEL QTY PROCESSOR UNIT FAULTY. REPLACED THE FQPU, ALL SYSTEMS CHECKED NORMALLY.

Part: SIGN — LOOSE (CABIN) · airframe 58,832 hrs · 19,889 cycles

DOOR 2L EMERGENCY EXIT SIGN LOOSE. REINSTALLED EXIT LENS.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 57,744 hrs · 19,680 cycles

SMOKE WAS DETECTED IN THE 2L LAV. 10-9-07 FLT ATTENDANT NOTED OVERHEATED ELECTRICAL ODOR IN LAV AT 2L UPON ARRIVAL; CAPTAIN CONFIRMED ODOR. TRIED TROUBLESHOOTING BY OPERATING ALL EQUIPMENT AND INSPECTING ALL COMPONENTS IN 2L LAV. FOUND ALL EQUIPMENT WORKING. NO ODOR DETECTED. POWERED AIRCRAFT AND COULD NOT DUPLICATE SMOKE ODOR AFTER ACFT WAS MOVED TO HANGER. INSPECTED INTERIOR LAV PANELS AND ABOVE CEILING PANELS AROUND LAVATORY. TURNED ON VIDEO SYSTEM, STILL NO DISCREPANCIES NOTED.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 56,458 hrs · 19,432 cycles

EMERGENCY EXIT SIGN L26 INOP. [SUP 06-06-07] REPLACED LIGHT SWITCH.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,458 hrs · 19,432 cycles

EXTERIOR EMERGENCY LIGHTS INOP AT DOORS L1, L2, AND 3L. [SUP 06-06-07] REPLACED BATTERY AND RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,458 hrs · 19,432 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

AFT CARGO STA 1420 LEFT SIDE FRAME HAS A DENT STR 27L. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN AND INSTALLED REPAIR ANGLE PER UA ENGINEERING SPECIFICATIONS.

Part: SKIN — GOUGED (LT WING) · airframe 56,458 hrs · 19,432 cycles

LEFT WING LWR SKIN FASTENER HOLE -B- AT SIDE LINK FITTING ATTACH AREA HAS 3 EA DEEP GOUGES. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN, REPLACED PRODUCTION SLICE AND REPAIRED HOLE PER UA ENGINEERING SPECIFICATIONS.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

FWD CARGO STA 600 LEFT SIDE FRAME DENTED STR 24L. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE SKIN, REPLACED PRODUCTION SLICE AND REPAIRED DAMAGED AREA PER UA ENGINEERING SPECIFICATIONS.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

LEFT FUSELAGE SKIN HAS 5 DENTS FROM STA 600 - 660, BETWEEN STR 17L AND 18L. [SUP 06-06-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND INSTALLED A DOUBLER REPAIR. THIS IS A TEMP REPAIR, LIMITED TO 12 MONTHS FROM 8MAY07, AND A NEW FAA 8100-9 MUST BE ISSUED PRIOR TO THAT TIME, IN COMPLIANCE TO 14 CFR 25.571.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

AFT CARGO STA 1440 LEFT SIDE FRAME HAS DENT STR 25L. [SUP 06-06-07] MAJOR REPAIR ACCOMPLISHED. SPLICED IN DOUBLER REPAIR, THIS IS A TIME LIMITED REPAIR FOR 12 MONTHS FROM 08 MAY07 UNLESS A NEW FAA 8100-9 IS ISSUED PRIOR TO THAT TIME IN COMPLIANCE WITH 14 CFR 25.571.

Part: STRUCTURE — CRACKED (DOOR) · airframe 56,458 hrs · 19,432 cycles

MED 2R FRAME IS DAMAGED. [SUP 06-06-07] HFEC INSP FOUND CRACK AT FWD FRAME UPPER HINGE CUT OUT. INSTALLED A DOUBLER REPAIR PER UA APPROVED SPECIFICATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

AFT PIT FLOOR PNL SUPPORT STR AT LBL 3 HAS CORROSION IN STA 1330 AREA. [SUP 06-06-07] FABRICATED REPAIR REPAIR VII. ORIGINAL MATERIAL 0.063, REMAINING AFTER CLEAN UP 0.044. INSTALLED REPAIR PER UA ENGINEERING SPECIFICATIONS.

Part: PULLEY — CRACKED (ELEVATOR CONTROL) · airframe 56,458 hrs · 19,432 cycles

CABIN CROWN AREA, 2 EACH ELEVATOR CONTROL CABLE PULLEYS ARE CRACKED AT STA 340 BETWEEN STR 2L AND STR 3L. [SUP 06-06-07] REMOVED AND REPLACED PULLEYS AT STA 340 AND VERIFIED CABLE TENSION. ACCOMPLISHED FUNCTIONAL CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,458 hrs · 19,432 cycles

LOWER FUSELAGE SKIN DENTED AT BS 480 AT STR 22R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED FILLER & INTERNAL DOUBLER REPAIR.

Part: UNKNOWN — UNKNOWN (NLG WARNING) · airframe 55,990 hrs · 19,342 cycles

ON CLIMBOUT, RECEIVED EICAS STATUS MSG: NOSE A-G DISAGREE. [SUP 05-18-07] CREW SAID, NOSE A-G DISAGREE DISPLAYED DURING CLIMB & REMAIN DISPLAYED, NO OTHER DISCREPANCY NOTED. REPLACED LT NOSE GEAR NOT COMPRESSED SENSORS

Part: SPRING — FAULTY (R4 DOOR) · airframe 55,616 hrs · 19,270 cycles

DOOR 4R HAS ARMING FLIP DOOR SPRING NOT HOLDING DOOR CLOSED. REPOSITIONED SPRING AND MADE READJUSTMENTS TO DOOR RIG. NO COMPONENTS REPLACED.

Part: CONNECTOR — BROKEN (CABIN) · airframe 55,616 hrs · 19,270 cycles

GALLEY 1B EMERGENCY LIGHT CONNECTOR BROKEN. REPAIRED EEL CONNECTOR.

Part: CYLINDER — OUT OF TOLERANCE (EVAC SLIDE) · airframe 55,616 hrs · 19,270 cycles

RIGHT & LEFT OFFWING SLIDE CYLINDERS ARE OUT OF TOLERANCE. RT OFFWING SLIDE CYLINDER LIMIT OVERDUE, DATE OF MANUFACTURE 4-92. CYLINDER NOT OUT OF DATE DOD, 26JAN07, BUT WILL NOT HAVE 20 MONTHS REMAINING. REPLACED CYLINDER. OPS CHECK SQUIB TEST FOR NORMAL READING.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 55,616 hrs · 19,270 cycles

LEFT SEAT 26 EMERGENCY LIGHT BULB MISSING. INSTALLED A NEW BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,616 hrs · 19,270 cycles

EXT EMERGENCY LIGHT AT DOOR L-4 INOPERATIVE. FOUND BULB INOPERATIVE.REPLACED BULB AND OPS CHECK GOOD.

Part: STATUS MESSAGE — ILLUMINATED (TE FLAPS) · airframe 54,441 hrs · 19,047 cycles

UPON PLACING FLAPS AT 5 UNITS, STATUS MESSAGE NOSE AIR GROUND DISAGREE DISPLAYED. MAINTENANCE EICAS PAGE SHOWED "NOSE GEAR LOCKED" AND "NOSE GEAR DOWN" MESSAGES. CLEANED NOSE GEAR SENSORS. BITE TESTED PROXIMITY SENSOR ELECTRONICS UNIT -NO PROBLEMS NOTED.

Part: WARNING SYSTEM — INOPERATIVE (FIRE WARNING) · airframe 53,693 hrs · 18,904 cycles

NO FIRE WARNING BELL DURING FIRE AND WHEEL WELL TESTS. RESET MASTER WARNING AND CAUTION SWITCH. CAPT AND FO SYSTEM OPS CHECK OK.

Part: BATTERY — DISCHARGED (DOOR 1L) · airframe 49,682 hrs · 18,127 cycles

EXTERIOR EMERGENCY SLIDE LIGHT IS INOP. REPLACE EEL BATTERY CHARGER AT DOOR 1L.

Part: LIGHT — OVERHEATED (ROW 10-11) · airframe 45,477 hrs · 17,104 cycles

SIDEWALL LIGHT AT ROW 10-11 LT SIDE EMITTING ODOR. REPLACED LIGHT ASSEMBLY.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 44,358 hrs · 16,721 cycles

FIRST CLASS EEL LIGHTS TURN OFF AFTER 1 MINUTE. REPLACED POWER SUPPLY & BATTERY PACK M732.

Part: PUMP — FAILED (LT ENGINE) · airframe 37,696 hrs · 14,228 cycles

LEFT ENGINE DRIVEN PUMP OVERHEAT LIGHT ILLUMINATED. PUMP DEACTIVATED, 30 MINUTES LATER LEFT SYSTEM LOST ALL FLUID. PUMP FAILED INTERNALLY. REPLACED LEFT ENGINE DRIVEN PUMP.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM WEB HAS ELONGATED FASTENER HOLES STA 324 RBL 43 WL 204. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS, ANGLE REPAIR AND DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

CABIN FLOORBEAM UPER SURFACE CORRODED STA 1681, STR RBL 12, RBL 24 TO RBL 30, WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLERS AND DOUBLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM UPPER CAP CORRODED STA 324, RBL 43-48. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FUSELAGE FRAME INNER FLANGE CORRODED STA 1640, BETWEEN STR 7L AND 8L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR TO FRAME.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 36,799 hrs · 13,917 cycles

RT WING TRAILING EDGE AFT FLAP DAMAGED. LOWER COMPOSITE INBOARD OF NR 7 FLAP TRACK TO LAST 2 INCHES OF TRAILING EDGE. BONDED IN FILLER AND BOTTOM LAYERS LAIDUP REPAIR PLYS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM CORRODED. STA 1681 RBL 24 TO RBL 30. INSTALLED T-CAP REPAIR WITH STIFFINERS.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

SHEAR WEB CORRODED. STA 1681 LBL 12. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM CORRODED STA 1681 RBL 32. INSTALLED T-CAP REPAIR AND STIFFENERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM CORRODED STA 1681 RBL 12. INSTALLED T-CAP REPAIR AND STIFFENERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOOR BEAM UPPER SURFACE CORRODED. STA 1681, RBL 12 AND RBL 24 TO RBL 30, WL 208. INSTALLED FILLERS AND DOUBLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM CORRODED STA 1681 LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND T-CAP REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOORBEAM UPPER SURFACE CORRODED. STA 1640 LBL 31 TO RBL 51 WL 208. INSTALLED T-CAP REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FWD PIT FLOOR SUPPORT INTERCOSTAL CRACKED. STA 663 RBL 19.8. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

CABIN FLOORBEAM CORRODED. STA 365 RBL 51 TO 70. SPLICED IN UPPER CHORD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FLOOR SUPPORT STRUCTURE CORRODED. STA 1673 WL 208 TOP AND BOTTOM SURFACE. REPLACED FLOOR SUPPORT STRUCTURE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

DOOR FRAME SILL SUPOORT CORRODED. STA 1645 RBL 52 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT CHANNEL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

FUSELAGE CREASE BEAM AND WEB CORRODED AT STA 934 STR 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB AND REPAIRED CREASE BEAM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

CABIN FLOOR CHANNEL UPPER SURFACE CORRODED. STATION 365.25 RBL 26.INSTALLED FILLER AND DOUBLER REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

INTERCOSTAL CRACKED IN AFT PIT. STA 1319 RBL 5 MAJOR REPAIR ACCOMPLISHED.REPAIRED INTERCOSTAL PER SRM 51-70-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

CABIN FLOORBEAM CAP CORRODED. STA 365 RBL 51 - 60. REMOVED DAMAGE AND INSTALLED NEW T CHORD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,799 hrs · 13,917 cycles

CABIN FLOOR INTERCOSTAL AT STA 365, RBL 42.45 CORRODED. REPLACED INTERCOSTAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,799 hrs · 13,444 cycles

DENT IN FUSELAGE SKIN. STA 615.REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,799 hrs · 13,444 cycles

DENT IN LT FUSELAGE TWO FEET FWD OF WING ILLUMINATION LIGHT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.

Part: TRANSMITTER — FAILED (T/E FLAP) · airframe 36,444 hrs · 13,784 cycles

FLAP CONFIGURATION WARNING ON TAKEOFF. REJECTED TAKEOFF AT 95 KTS, FLAPS AT 15. *S/D* FAILED RIGHT TRAILING EDGE FLAP TRANSMITTER. REPLACED SAME AND OPS CHECKED NORMAL.

Part: RADOME — BIRD STRIKE (NOSE) · airframe 33,243 hrs · 12,632 cycles

RETURNED TO EWR DUE TO A BIRD STRIKE. *S/D* ACP BIRD STRIKE AND OVERWEIGHT LANDING INSPECTIONS. REMOVED AND REPLACED NOSE RADOME DUE TO DAMAGE. ALL ELSE CHECKED OK.

Part: HOSE — RUPTURED (MLG ACTUATOR) · airframe 33,067 hrs · 12,563 cycles

LOST ALL LEFT SYSTEM HYDRAULIC FLUID AND ASSOCIATED SYSTEMS. RETURNED TO SFO. *S/D* LEFT MLG DOWNLOCK ACTUATOR HOSE WAS FOUND LEAKING. REPLACED HOSE.

Part: WARNING — ACTIVATED (4L DOOR)

ABORTED TAKEOFF AT 100 KNOTS DUE TO DOOR 4L UNSAFE INDICATION. *S/D* CHECKED DOOR PER MEL5271C AND FOUND TO BE SECURE ON INSIDE AND FAIRED ON OUTSIDE. NO OTHER ABNORMALITIES FOUND.

Part: TIRE — FAILED (LANDING GEAR)

RETURNED TO DEN WHEN BLOWN TIRE CAUSED FLAP DAMAGE WITH LOSS OF SYSTEM HYDRAULICS. *S/D* REPORT FROM BRIDGESTONE ACFT TIRE, INC. TIRE SUFFERED A 3 PIECE FLEX BREAK (2 SIDEWALL/BEAD SECTIONS AND 1 CAP SECTION) DUE TO POSSIBLE RUNNING OF TIRE WHILE UNDER INFLATED. CONSIDERABLE CORD FRAYING THAT WAS EVIDENT SHOWED LONG TERM EXPOSURE TO EXCESSIVE FLEXING (UNDERINFLATION). THERE IS THE POSSIBILITY THAT FOD CAUSED THE DAMAGE. REPLACED WHEEL ASSEMBLY.

Part: VALVE — FAILED (APU)

APU BLEED VALVE WOULD NOT OPEN. APU BLEED VALVE IN CLOSED POSITION, AND APU BLEED POWER CIRCUIT BREAKER IS SAFETIED OPEN. *S/D* REPLACED APU BLEED VALVE PER MM 36-11-10, OPS CHECKED GOOD.

Part: ACTUATOR — DEFECTIVE (LE FLAP)

LANDED IN SFO UNDER AMBER ALERT DUE TO A LEADING EDGE FLAP INDICATION PROBLEM. DISCOVERED FAULTY LEADING EDGE SLAT ACTUATOR. REPLACED ACTUATOR. OPERATION CHECKS NORMAL.

Part: AIR DISTR — ODOR (COCKPIT)

STRONG ODOR IN COCKPIT AND CABIN, FLIGHT DIVERTED TO ORD.

Part: SLIDE — LEAKING (DOOR 4R)

DOOR 4 RT, RETURNED TO SHOP FOR TIME CONTROLLED OVERHAUL. THE LOWER INFLATION TUBE IS LEAKING AT THE SEAMS. ALSO, THERE IS CORROSION IN BOTH ASPIRATORS AND ON THE CHECK VALVES. RETURNED TO VENDOR FOR REPAIR.

Part: SMOKE DETECTOR — INOPERATIVE (AFT LAV)

LAVATORY SMOKE ALARM WON'T TURN OFF. DEBRIEF CABIN CREW FOR SPECIFIC LOCATIONS. SMOKE DETECTOR INOP IN AFT LAV, SYSTEM OP CHECKED OK. SUSPECT PASSENGER BLOCKED OFF DETECTOR.